SCIENTIFIC ABSTRACT KIRILLOV, I.A. - KIRILLOV, I.I.

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• Collection: Scientific Abstracts
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• Document Creation Date: November 2, 2016
• Document Release Date: September 18, 2001
• Sequence Number: 18
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

KIRIIWTr-" , prof.1 BORODIN, S.V.,j TiVoOR, R.D,; TOSYMSENS11Y, A.Ae;
GIROVSKIY, T.Jr.., ZHITOMIRBIJY, N.G.; SAFRAY, G.Te.; SICHII, XOGS;
NIKITIM, N&D.; YILATOT, X.L.0; FIAIXOTA. T., red.; LUX=, Ae~
takha.red,
[finances of branches of the national economy] Yinaney otraelei
narodnogo khoslaistya. Avtorskii kollektiv pod rukoTodstvou
L.A.Kirillova. Xoskya, Goofinizdat, 1938. 302 p. (KIRA 12:2)
(finance)

KIRILLOV, Ivan Akimovich, prof.. Prinimal uchaotiye GIROVSKIT. T.Y.,
oty.red.; YILIMVA, Z., red.isd-va;
LZBZW, A., takhn.red.
Dinances of socialist industry] Finanny sotsiallatichookoi
promyshlonnosti. Xoskva, Goofinisdat, 1959. 279 P. (KIRA 12:10)
(Finance)

KIRILLOV, 1. F.
Kirillov, 1. F. "Surper plantirr- of potatues with freshly-harveste tillb,=- in Tadzhiki-
stan", P,)T.Ileten' po plodovodstni) vinogradarotv,; i No. ~) P. ll-~O)
Bibljo:~: 16 items.
SO: U-);392 IP Auru3t 53, (Letopis 17hurnal In,,,kh Statey, l1r) 21, 111-licl).

KI ki L- L-0 V / - r.
-:11MMM I --I. -F.
Klrdllov, 1. R.% -Conditions and immediate tasks of winegrowing in the
Tadzhik S^3R", Byulleten' po plodovodstvup ovoahohavodt;tvu i vinogradaretvu,
No. 9, 1948, p. 3-19.
SO: U-3042, 11 March 53t (Letopis Inykh State.y, No. lo,,1949).
, ~ va

KIRILLOV, I.F*
Kulltura vinograda i ego agrotekhnika
v Tadzhikskoi SSR (Cultivation of the grape anI its
agrotechnolojV in Tadzhikistan). Stalinabad, Tad-
zhikgosizdat, 1952. 120 p.
S3: Monthly List of Russian Accessi-ons, vol. 6, '.*o. 1, April 1953

KiRI ---:,IV, I.F.
"The oultivotiin of p3tvtoos in Tsdzhikiqtan." Acsdl Sc:i Tmdzl~:'~- ll.~R.
Deportripnt )f Natural Sciences. StjUnabod, 1356
Mosertatt,)n for the Degree of CanclLdsto ;.n AgricuLtursl Jcle~naaj
ji: Knizimayik iotopinl, N'. 1.4, 1956

USSR/Cultiva",(~~. - P)t0tocs, I!c.-,:u.'-nblco, Mclonw.
Abs Jour -".tu- - Diol,) ],',i C,; "!~, 2
Aut2iGr Xil-illov, I.F.
Inat
Titlo : T -.c A, X itacliny o f Larly 11i Ca Yielclill Itot -)c 0
(A,i,,* Pul,: lnw~zmlzintmm, ,i) 2, 4o-45.
Abstract : Lifluonca of tLa -.ize ).' the tubers, of t:,r-,i:- vunia-
1L.*"tio;I, of soil jxcparntioll, of tillili~;; milek L)~^ :..C-
L:~v,-In, o.- plantiur; un tho yW10. u.' potnto crops Li T"-Oji-
!-.iuta:, is cleacribc,-'. 12',o results were -j*()tvii,.c-(' by
utilizia.,, larLp anO. uize vernalizoa tifoers Cu~--
Lir, fnll plusdii(; at ~i 27-30 cu anc! Cmria,;
:,.arrowin~;. The ii. pot--t:)cs carly alit.!
VIL~1.1 z~%laas --f 70 x W cu in 11--)tc.'. --
Cnra 1/1
6-3 -

KIR t-I-F.; RYBNIKDV,, A.A.
The roaring forties, Priroda 52 no,042-47 163, (MIRA 1614)
1. Goeudarstvennyy okeanograficheakiy institut, Moskva.
(Antarctic regions)

I
KTRTLLOVt LIF,
I
Tieing the nxT&rlnul method for OalTilatirg the r'sc and flvv os-
cillationo In the lovel of tho Sea of Azov. TrLdy GDIN nc.75:43-
48 164. (MILRA 17t10)

-- N~~
K -Z-K -F/-/- (4// -Z--; Z-!-
ZASLAVSIIY. Yu.S.; SHOR, G.I.; KIRIIMV. 1.G.; IMMIVA. 7.B.; TEVSTIONMY,
Te.Y.; ZLOBIX. 0.A.
Using radioactive tracers (tagged atoms) for studying wear
properties of lubricants. Trudy VNII IIP no.6:58-84 157. (KRA 10:10)
(lubrication and lubricants) (Radioactive tracers)

ZABLOMM, Yu. S.; SHCO, 0. 1.. G.; 113MA, 1. D.; 17 GISM, To. V.;
mA ZMM, 0. A.
"Tbe Application of Badloactive Indicators (Tagged Atom) in the 1wrestigation
ofieer Posistant Properties of Lubrloating Oils." P. 58.
in book Study and U" of Petroleum Products, Mmoov GostoptekhIzdat, IZ7. 213pp.
MWS ooneotion of articles gives results of scientific research vork of the An-Won
Bolgiif Ic Research Inst. for the Processing of Petroleum wA Ges for the ProdVotion
of Synthetic Liquid Fuel*

KIRILLOV,, I. I.
"Thecxy and Design of Steam Turbines)" 19h7

KIRILDOV, I
PA 37/49T18
Jul/Av4AS,
Turbines' Stem
"Letter to the 3di.tor on ShlrItekly's Nerlew-of TheLr
Book," 1. tIrIllor, S. Antor, P
No 4*
Apology to Zhiritskljr for accidental =lesion of
aokncn?lodgement of use made, of ZhIrItakiy's work
(see 3TA9Tiq),#
STAWIS"

KIRILLOV, 1. 1.
"The Force of Social Reactionp" Morskoy Flot., No.h. Jqh8
Chief Scientist, Main Admin. Cadres W

KIRILI,)V, LT.
Gazovyc turbiny. Moskva, Mashgiz, 1949- 386 p., diagys.
"kniga osnovana na kursakh lektsiip ctitannykh moiu v LeninLraeskom politekhniche-
skom institute." P-3.
Title tr.: Gas turbinese Aviation gas turbines; p-332-34h.
TJ778,K5
SO: Aeronautical Sciences and'Aviation in the Ooviet Unions Library of Congresss
1955-

IIRILWV I.I., professor, laureat' Stalinskoy premil, redaktor; LURIYX,A.I.,
- WWWAWM
ifift'geor'~-edaktor; POLISNATA, P.G., takhalcheskly redattor.
(Strength of steam turbine elements; a collecton of articles] Prochnost'
elementov parovykh turbin; sbornik statel. Koskya, Cras.nauebno-takhn,
Izd-vo mashinostrott.lit-ry, 1951. 242 p. 191crofilml (KLRA 10:4)
(Steam turbines)

1. T
.PHASE I TREASURE ISLAND BIBLIOGRAPHICAL REPORT AID 259 - I
BOOK Call No.: AP579436
Author: KIRILLOV, I. I., Professor in the Bezhitsk Institute of
-Transportation-Machine Construction
Full Title: REGULATING STEAM AND GAS TURBINES
Transliterated Title: Regullrovanlye parovykh I gazovykh turbin
Publishing Data
Originating Agency: None
Publishing House: 3tate Energetics Publishing House (Gosenergoizdat)
Date: 427
1952 No. pp.- No. of copies: 7,000
Editorial Staff
Editor: None Tech. Ed.: None
Editor-in-Chief: None Appraiser: None
Text Data
Coverage: This book Is a further development of the monograph Automa-
tic Devices for Steam Turbines published in 1938 whic as
a compilation of a numBer -3-f-papers written by the author
for engineering-technical courses held by the authors in
plants and institutes of the turbine-construction industry.
It contains a description of the theory of machine regula-
ting systems and an analysis of applicable governing eystas,
and of the construction characteristics of basic components
of these systems. The statics of governing is described In
the first part. The general theory and methods of study of
governing processes, and a number of Individual governing
1,72

Reguliroveniye parovykh I gazovykh turbin AID 259 - I
problems (influence of friction, delays, etc.), are de-
scribed in the second part. Basic Iftformation on govern-
ing systems and security devices of contemporary steam
turbines are described in the third part. The dynamics of
open-type gas turbine governing is shortly described in
the fourth part. Diagrams, graphs.
The book is interesting because it contains descriptions of
a number of regulators of Russian design, and a number of
charts representing tests with these governors.
Purpose: A textbook for students of Institutions of Higher Learningo
and also for engineering and technical workers who design and
operate steam and gas turbines.
Facilities; A considerable number of Russian scientists, research insti-
tutes, and industrial plants are mentioned In the text.
No. of Russian and Slavic References: 25 before 1939, and 41 after this
date.
Available: A.I.D., Library of Congress.
2/2

. w
KIRILLOY. 1.L. doktor to choskikh n&uk. professor.
I- , OUM%,..
On the 200th anniversary of the publication of lulorfv~worke on
the theory of turbomachinse. Trudy Bosh. inst. trausp.mashinostr.
no.15:3-4 153. (nU 10; 2)
(Xuler. loonhm,4, 1707-1783)

LLOV, I.I., doktor tokhnlcheskikh nauk, professor.
Ways of Increasing the efficiency of steam turbines. Trudy Bosh.
inst.tr"sp*uashinostr.no,15:5-10 '55. (MM 10:2)
(Steam turbines) '

XIRILLOVO IIL, doktor tokhnicbeskikh nauk, professor.
'_---'-~~;thod for designing the flow are& of turbines with twisted blades.
Trudy Ush.lust.tranap.mashinostr. no.15:11-21 '53. (MM 10:2)
(Steam turbines)
.1

KIRILLOV, 191., doktor tekhnicheskikh nauk, professor.
Zxperimental singlo-stage air turbine in the turbine laboratory
of the Beshitskil Institute of Transportation Nachinery Manufactw-
ing. Trudy Bash.inst.tranap,mashinostr.no.15:46-30 '55. (MLRL 10:2)
(Air turbines)

MILLOV, ILLe, doktor tokhnicbeskikh nauk, professor.
Zffect of initial and final parameters on varying consumption of
steam or gas in turbines. Trudy Bosb.inst.tranap.mashinostr.no.15:
61-70 155. (MM 10:2)
(Turbines)

KOVAIRTSIXT, Mikhail Mheylovich; MIUA- ~ h W doktor takhaichookikh
nauk, retsensent; XWINSKIT. G.K., ins-f*-nor, retsanxent; BITMV,
B.L., Inzhener# redaktor; DUGnA, N.A., tekhnichaskiy radaktor
Dteam turbines; a popular scientific sketch] Phrovye turbiny;
nauchno-popultarnyt ocherk. Moskva, Goo. nauchno-takhn. Isd-vo
mashinostrolt, lit-ry, 1956. 102 p. (MLRA 10:2)
(Steam turbines)

26(l) PHASE I BOOK EXPIDITATION SOV12116
Kirillov, Ivan Ivanovich, Professor (Bezhitsa rnstitute of Transportation Machinery
Rffu-f~-c ~ur ng~~'
Gazovyye turbiny I gazoturbinnyye ustanovki, tom 2: Gazot-urbinnyye ustanovki
(Gas Turbines and Gae-Tarbine Uaits, Vol 2; Gas-Turbine Units) Moscow,
Mashgiz, 1956. 318 P. Errata slip inserted. 7,000 copies printed.
Reviewers: S. A. Kantor, Professor, and A.A. Kanayev, Candidate of Technical
Sciencee; Ed.: R.M. Yablonik, Candidate of Technical Sciences; Tech. Ed.:
B.I. Model'; Managing Ed. for Literature on Transportation Road, and Power
Machinery YfLnufacturing: 0.1. Petrov, Engineer.
PURPOSE: This is a textbook approved by the Main Administration of Polytechnic
and Mechanical Engineering Vuzes for students of mechanical engineering vuzes.
It may also be useful to engineers designing gas-turbine units.
COVERAGE: This second volume of the author's monograph on gas turbines contains
basic information on the work of a gas-turbine unit. It Is supposed that the
reader is familiar with elementary prob1cme of the theory of turbomachines.
The book deals primarily with the investigation of the thermodynamics of gas-
turbine units, their operation under various conditions and their regulation.
Card 1/8

Gas Turbines and Gas-Turbine Uaits SOV121-16
A brief analysis and description of the basic types of Stationary and mobile
gas-turbine units are given. Special consideration is given to light gas-
turbi.ne units. Turbojet engines are mentioned only briefly as one of the ex-
amples of light gas-turbine power units. Some consideration is given to heat-
exchange apparatus. No persona.Uties are mentioned. There are 67 references:
33 Soviet, 27 Englifsh and 7 German.
TABLE OF CONTENTS:
Fbreword 3
Symbols 4
PART I. THEWDYNAKCCS OF GTU` (GAS-TURBINE UNITS) AND
HUT-E)MRANGE APPARATUS
Ch. I. lbeory of Gas-turbine Units With Continuous Combustion 7
1. Ideal cycle 7
2. Cycle of a real gas-turbine unit 13
3. Regenerative cycle 21
4. Yantbexmic compression and expansion 25
card 2/8

Gas-Turbines and Gas-Turbine Units SkN/2n6
5. Intercooling 34
6. j?eheat 37
7. Corrections for the internal efficiency of gas-turbine units
with swIl variations of parameters 43
8. Effect of resistance in conduits and in heat-exchanging apparatus
on the efficiency of gas-tarbine units 48
9. Effective efficiency of gas-turbine units 55
10. Closed cycle
Ch. 171. Theory of a Gas-Turbine Unit With Interlzdttent Combustion 61
11. Cycle of 3r ideal gas-turbine unit with intermittent combustion 61
12. Flow of gas from a closed chamber 63
1i. U,,eful vork coefficient 66
14. Heat process taking into account turbine and compressor losses
and the preheating of compressed air 67
15- Comparison of gas-turbine units with continuous and inter-
mittent combustion 70
Ch. III. Combustion Chambers
72
Card 3/8

Gas-Turbines and bas-Turbine Units SOV12116
16. Basic requirements 72
17. Process of combustion 73
18. Designs of combustion chambers 77
19. Fuel and fuel supply 83
2o. Combustion of solid fuels 86
Ch. V. Calculation and Dusign of Air Preheatera 94
21. Heat transfer and resistance in air preheaters 94
22. Example of air preheater calculationa 98
23- Influence of basic paramete-1-s on the dimensions of the
regenerator 102
24. Design of regenerators 107
PART 2. FERFORVANCE UMER DIMHENT OPERATING CONDMONS
AND-REGUIATION OF W-TURBINE UNITS
Ch. V. Statics of Regulation no
25. Methods of regulating gas-turbine units 110
26. Basic requirements for gas-turbine units and problems of
regulation 120
Card 4/ 8

Gas-Trabines and Gas-Ttwbine Wits SOV/2116
27. Control system 123
28. Yethods of changing the speed of rotation and the load 129
29. Static characteristics of regulation 133
Ch. VI. Dynamics of Regulation 137
30. Small vibrations 137
31. Equations for the rotor and governor 139
32. Stability of regulation A5
33. lb-regulation :L48
34. Protective apparatus of gas-turbines 156
Ch. VII. Work of Various Types of Gas-turbine Units Under Partial Loads 158
35- Single-shaft gas-turbine =it without regenerator 158
36. Influence of the regenerator on the operation of gas-turbine
units under partial loads 168
37. Two-shaft gas-turbine unit with separate compressor 170
38- Influance of intercooling and reheat on the operation of a
two-shaft, ips-turbine unit under partial load 178
39. Two-shaft gas-turbine unit with separate compressor drive 182
40. Closed gas-turbine units 194
Card 5/8

Gas-Turbines and Gas-Turbine thits SOV/2U6
PART I1X, GAS-TURBIB US=
Ch. VIII, Stationary Gas-tumbine Units 207
41. Single-sbaft ps-tiwbine units 2W
42. !Vwo-sbart gas-turbins units 215
43. Closed units M
44. Semiclosed units 231
45. CoMaxison of economic indices of steam and gas turbines of
electric power stations 2"
Ch. IX. Gae-Turbine in the JbtallurgLcal and Chemical Industries 236
46. Gas-turbine for driving blest-furnace air-blowers 236
47. Air turbines for blast-furnace air-blover units 238
48. Gas-turbines for petroleum refineries and nitric acid
production 245
Ch. X. Gas-Turbine in Combination With Steam Power Unit 247
49. Gas and steam turbine unit 247
Card 6/8

Gas-Tarbines and Gas-Turbine Units SOV/2i16
Ch. XIV. Yarine Gas-turbine Units 301
60. Requirements for marine engines 301
61. Design features of marine gas-turbine units 302
62. Economic indices of different marine units 309
BiblAography 311
Subject Index 313
AVAIIABIZ: Library of Congress
IM/fal
9-9-59
Card 8/8

A4AjkWj..j" professor; XOM, B~Ao, professor, retseassAt; XMYN, AmA*g
kandtidat takhalchookikh nauk; 'retsessentIJAMNIX, RX, kwdldat
takhnidhosldkh sank, redaktor; NDMLI B.I., takhnichookly redsktor,
(Gas turbines wd gas turbines installationslGaseTys turblay i gazo-
turbinnyo ustanovki. NeskTa, Ges.wwchn*-tekhn.lzd-To mashinestrolt.
lit-ry. Tol.I.CG&s turbines and compressors) Gasovyo turbiny i ken-
pressory. 1956. 434 pe Oa" 9W
l.Beshitaki.r Inst1tut transportnogo mwhinostroyenlys, (for Urillov).
(Gas turbines)

XAVAIIV, Audrey Andreyevich-, IOM, A.P., akademik. reteensent! Xj%4LIQj,
I.I., professor, doktor takhnichookikh nauk, radektor; STIPAICHINKO.
r6dalctor I%d&tal'StVal TIOANOV, A.Ys., takhnichaskiy rodaktor
(Yrom water mill to atomic sngIns3 Ot Yodianol mallnitay do otomnogo
dvigatelia. Izd. 2-oo, dop. Moskva, Goo.nauchno-takhn., isd-vo
mashinostroit. lit-ry# 1957. 231 P. (KLRA 10:9)
(Angi no a )

312
Kiri-llov, I,Jp, Professor, Doctor of Technical Sciences and
Ya-V1-0-n1Z,'-Y--M., Candidate of Technical Sciences.
The influence of closed axial gaps on the efficiency of
active type stages with cylindrical blades. (Vliyaniye
zakrytogo osevogo zazora na k. d. stuponey aktivnogo tipa
s tsilindricheakimi lopatkami.~'
BRIODICAL: "Diergomashinostroenie", (Power Machinery Construction),
1957, No. 5, pp. 15 - 18, (U.S.S.R.)
BSTRACT: Until recently, small closed axial gaps have been used in
active type stages of steam turbines'and sometimes also in gas
turbines. Numerous experiments carried out in the Bryansk
Institute of Transport Engineering as well as theoretical
considerations show that the application of quite long closed
axial gaps in active type stages can be very useful in
increasing both the reliability of the blading and the stage
efficiency. The gaps are classified as follows: a front open
axial gap between the edge of the shroud and the body of the
diaphragm, the back open axial gap, the closed axial gap
bounded by the cylindrical solid wall of the fixed diaphragm
and the closed axial gap formed by the overhang of the shroud.
Another important gap is that between the outlet edges of the
guide vanes and the inlet edges of the working blades. This
gap and the closed axial gap bounded by the cylindrical walls
are the subject of this article. Investigations on stationary

The inf'lu~~-nce of closed axial Grips on the efficiency of312
activ,~ typc stages with cylindrical blades. (Cont.)
bladinG were made long ago, and the existing situation is
reviewed. Xhese wece concerned only --.vith profile energy
losises and did not allow for friction on thu walls bounding
the closed axial Cap. In a tul:-binu C-Lage there are a number
of efi'ects adlitional ~,o those that occur in stationary blading
which can cause vital changes in Uh--~ energy losses. The most
imporUant L;peclal f,.,aturcs introduced by rotution of the rotor
aru conside.-ed, and a foiiatila 1:3 derivud for tile pressure drop
due to friction in a closed axial gap. Fro.,.i this a formula is
derived for tile influcnce of th~~ dogr,.,e of reaction on the
~;nerGyloss- by friction in tho clo"sud Gap. Pro;-.,. this formula,
i~, follows, for oxaiiple, thaU when the degree of i-eaction is
0.5, i;he friction loss,-;b related to th,,~! total heat drop are
only half tho:~a when there is no reaction. In order to give
some idea of tile magniLude of Uht-. efficiuncy chanr-,-.s under the
influence of a ciozed axial jap, examDle-- ai-e Given of tests
on models of aculvo type turbine z-ta6~es ~,,ith difft~rent heights
and Made profilL;s. The toots weixi mlade orl experimental
turbines opui-atin:r on air. Curvus ave -ivon of the efficiency
for various icnb-ths of clo:-,ed a.-;--ial As tile 1-,2nGth of th(
cloz--ad aXial L;ap is increased tht-, curveS bt--,com~ zom-zwhat flatt(
Similar tust.- are madl(~ various bl--de des-',L-,ns. From the
experim---nUal results und the theoretical c on--ide i-at ions that
accompany them it follows that it is advantageous to make the

312
The influence of closed axial Caps on tho ef-l'iciency of
active type stages with cylindrical blades. (Cont.)
cl,joed axial gaps relatively great for staGes with both
relatively short and relatively loi% blades. Taking into
account that for stages with loner blades the positive influ-
once of increasing the axial Gap in cqualisinr- the forces acting
on the blades assumes special importance .he value of using
lonG closed axial Fpps which sii:~ultaneously increase the
efficiency becomes evident.
On the other hand as the closed axial Gap is increased there
is a change in the structure of Lhe flow and in the field of
pressure before the workinG wheel and, because of this, there
are also changes in the leakage of Lteam through the open axial
gap. The influence of various desiGn factors on steam leakage
is explained.
"Some tests were made with verj closed gaps (above
100 nutis) in order to get some idea of the friction. In this
re-ion, the influence of flow equalisLation b,~-comos negligibly
small. The results of the tests a..v showm in the graphs.
The experiments carried out i:,,akc it possible to evaluate
appioximately the energy losses due to operaticn of the
bladinG in a non-uniform flow.
The followinf- practical conclu-sions are dra-,n from, the
viork. At Lhe present time in dossiLgiin,,.- a -tive type sta6es of
steaii turbinus tile distances between the cdr;es of the guide

Tile influence of closed axial Uips on the efficiency-o-r
active type stages with cylindrical blades. (Cont.)
and viorkinG bladinG are often made small. Numerous tests
that have been cai-ried out show Lf-iat it is advisable to use
comparatively large axial gaps. The tests established that as
the lenELh of the closed axial tLap is increased, provided that
the blading is lonG enough, the of.Ciciency first increases
considerably, then reaches a madivu!;i and then slowly falls.
Tile length of closcd axial F;ip siliould, Wierefore, be selected
at not lesi; than the value corresponding to may-imum efficiency
as shovm. in the experimental data. The increase in efficiency
associated virith equalisation o-C thu flo-w., and, v,-Ith sufficiently
long, bladin(wj the maximum efficiency, are in the regions where
the flow is well equalised. Therefore, the selection of a
lar6e closed axial gap leads no-; only to some increase in the
stage efficiency but also increaces the reliability of the
turbine reducing tile probabilit;,y of blade vibration. From
this poinL of view, with Ion- bladinC, iL may be advisable to
select a closed axial &ap somewhat lon6er than the optimum
value from the standpoint of efficiency. It is particularly
advisable to use lon,- closed axial k;aps in turbines with a
wide range of speed, for instance in rLarina turbines and in
turbines for driving blowers, since when the stages operate
with large angles of attack the gain in efficiency from the
application of lonh~ axial 6ups increases. Besides, for
turbines of this type, the selection of long axial E;aps is
also very useful from the point of view of blading strength.
8 figures, 5 literature references. (3 Russian).

10(2) PHASE I BOOK EXPLOITATION SOV/1308
Kirillov. Ivan Ivanovich, Rakhmiyel! Mordukhovich Yablonik, Lev
~-Vasfl'yev-139-19-"T -ev, Ivan Grigorlyevich Gogolev, Ryurik
Vladimirovich Kuzimichev., Gennadiy Ivanovich Khutskiy,
Rostislav Ivanovich Dlyakonov, Viktor Dmitriyevich Pshenichnyy,
and Aleksandr Aleksandrovich Tereshkov
Aerodinamika protochnoy chast! parovykh i gazovykh turbin (Aerod)namics
of Steam and Gas Turbine Flow-Pas8age Areas) Moscow, Mashgiz., 1958-
246 p. 4,500 copies printed.
Ed.: Kirillov., I.I., Prof essor,Bryansk Institut of Transport Machine
Building; Reviewer: Shubenko,, L.A., Corresponging Member, USSR
Academy of Sciences; Tech. Ed.: Gerasimova, D.S.; Managing Ed.
for Literature on General Telhnical and Transport Machine Building
(Mashgiz): Ponomareva, K.A.. Engineer.
PURPOSE: This book was writter, for engineers working on the design,
Card 1/6

Aerodynamics of Steam and Gas Turbine Flow-Pas3age Areas SOV/1308
manufacture and operation of steam and gas turbines. It may aloo
be useful to students of special courses.
COVERAGE: The Withors analyze' phys 1ca 1 phenomen4, connected- with flow
through the stages of imphlee steaia and gas'turbines. They give
the results- of experimental invastigation of stages with full and
partial supply of the-working medium. -The basic results obtained
are for high "-and medium-powerpd turbines.
Results of the Investigation of a new low-powered turbine are
also given. Practical recommendations for the design of the flow
passage area of steam and gas turbines are given, based on the
investigation of effect of various design measures on the efficiency
coefficient of stages. The Investigation was made in the BITM
(Bryansk Institute of Transport Mchinery Building). The following
sections were written by members of the Chair of Turbine
Construction of the BIT14: PrDfessor I.I. Urillov, Docent,
Candidate of Technicdl Sciences, paragraphs 1, 2, 13o 16; Docent
Card 2/6

At:-rGdynamics of Steam and Gas Turbine Flow-Paneage Areas S 0V i -'j C, " '~'
R.M. Yablonik, Candidate of Technical Sciences,paragraph 9; 1.1.
KIrJllov and R.M. Yablonik, paragraphs 304, 5; L.V. kirtsev,
Cand-f.date of Te,I-hnIcal Sciences., paragraphs 6,7, 19; L.V. Gogolev,
Candidate of Technical Sciences, paragraphs 10, 11; R.V. Kuzlmichev,
Candidate of Technical Sciences, paragraph 8; G.I. Khutskly,
Candidate of Teohnical Science, paragraphs 12, 14, 15; R.I.
D' yalmov , paragragh .17; V.D. P3henIchnyy . Engineer of the Kirov
Plant, paragraph 1 ; A.A. Tereshkov, Engineer of BITM, paragraph
26'. The Leningrad Metal Plant, Kharskov Turbine Plant, Kabush
Plant and Leningrail-Ktrov Plant contributed to the develop-
neat of -?xperimental workz-- -~ ','!irbInes for BITM. The bibliography
of 2*3 references. I'- of which are Soviet, and 1 is German.
TABLE OF CONTENTS:
Preta,~e
3
Card 3/ 6

Aej,,,-)dyr!amIc,,3 of Steam and Gas Turbine Flow-Passage Areas SOV/1 3 Ot'i
-;4-p,-i I Sy
~mbuls
Ch Fxp-.--rIm&ntaI Stands and Te3tijig Methods
I. Pvoolerns of experimentr-I testing of the flow-pas8age area
c,f a E.-xr-blne
2. New air breathIng exper.Lmental turbines 12
3. M,~thod of investigating rotating mcdels of turbine stages 2-1
Ch. 1T. Stages With a Full Supply of the WorkIng Medium 39
4. The degree of reaction and the eecape of steam in stage-9
of an impulse type 39
Effe,-,t of special design features of impulse turbine
sr-ages on losses of energy 56
6. Strocture of the flow in open axial clearances ir, a
3tage of an impulse turbine 84
7. SO-,--cbure of the flow with steam induction at the root
of an impulse stage -97
card 4/ 6

0
Aerodynamics..of Steam and Gaa TLu-binc F16*-Pasi;age Areas SOV11308
8. Investigation of the three-dimensiorkal flow of gas in
a turbine stage with b).ades profiled according to the
law expressed by Cuj-fzCDS2O( - const. 101
9. Work of turbine stages in the region of saturated steam
and problems 6f investigation. 119
Ch. III. Stage With Partial Admission of the Working Medium 131
10. E%perimental investigatl.~.,-.-, of physical processes in the
flow behind the part'LL11. nozzle apparatus 131
11. Some reBults of tests o 7,artial stage models 143
12. Choice of optimim comb ~-on of active nozzle curves in
groups of partial sta.,,!.; 159
Ch. IV. Exhaust Losses 165
13. Reducing exhaust lossez, pressure and gas turbines 165
14. Effect of the nonunifo,-,i,!',~~i of the inlet profile of
velocity on the work of i,t,- turbine stage 173
15. Use of exhaust kinetic onori:j in the intermediate stages
of a multista& turbin,~ 181
Card 5/6

.Aerodynamicz of Steam and Gas Turbine Flow-Passage Areas SOV/1308
Ch. V. Low-powe'r Turbines . 194
16. Radial centripeta'.1 tvrbi-ne with internal partial supply
of steam 194
17. Experimental investigation of a centripetal turbine with
internal partial a-team supply 203
Ch. VI. Laboratorj Equipment 223
18. Experimental press-ire turb'nes 223
L
19. Exper�enee working with an aerodynamic angle-gage 238
20. Experience manufacturing silioon-aluminum blades 240
Bib'llography
AVA,IIABLE: Library of Congress
IS/ksv
3-17-59
246
Card 6/6

SOV/96-58-11-21/21
,IXTEOR: -Zirillov, I.I., Doctor of Technical Science
TITLE: Concer-ni-n-,g--S.,i-.,iksyutiii's Book IThe Future Development
of Steam and Gas-Turbine Electric Power Stutions,
Mexhgiz, 1957 (0 knige S.A.iJ-,syutina "Perspel-tivy
razvitiya parovyk-h i gazovyl-h. turbin elektriches7,7ikh
startsiy' I Mashgizj 1957. ?19 str.)
PE-111IODICAL: Teplo~!nr!rg,
'r 11, pp 94-0 (USSR)
,til-aj 1958,,E 96
ABSTILWT: Th,-~ gr!nerul criticism, th~4 the! book has an academic
approach, issupported by a number of exumples.
sn,veral errors in thp book a-.:e pointed out.
Card 1/1

---8(6) SOV/143-58-11-15/16
AUTHORS: Kirillov, I.I., Doctor of Technical Sciences, Profes-
-
sor, X-ir-ill-o
v, A.I.
TITLE: The Influence of Experimental Turbine Vibration on the
Test Accuracy
PERIODICAL: Izvestiya vysshikh uchebnykh zavedeniy, Energetika,
1958, Nr 11, pp 116-125 (USSR)
ABSTRACT: The rapid development of power engineering in the USSR
requires experiments for improving the flow area of
different turbine designs. Contemporary requirements
for the accuracy of aerodynamic experiments are very
high. Deviations of test data obtained by using the
same experimental unit often cannot be explained by
errors of the aerodynamic and other instruments used
for the experiments. These differences reduce the con-
fidence in utilizing experimental data which decreases
the effectiveness of the very important and complicat-
ed experimental work. At BITM those physical phenome-
na on experimental turbines were inventigated which
Card 1/5 may cause errors in the test results and which frequent-

SOV/143-58-11-15/16
The Influence of Experimental Turbine Vibration on the Test Accuracy
1y escape the attention of the experimental investiga-
tor. The explanation of mechanical vibration losses
is a part of this investigation. The influence of
such losses cannot be avoided completely and sometimes
it attains a considerable importance, since experimen-
tal turbines work in a wide range of velocities and
are equipped with numerous devices having different
self-oscillation frequencies. The authors present in
this paper some theoretical considerations and results
of special experiments explaining the origination and
possible magnitude of mechanical energy losses caused
by vibrations of the experimental turbine. Without
going into details with explaining types of experimen-
tal turbines, the authors investigate a very simple
system which is common to all machines. It consists
of a rotor with the working wheels at one end and the
braking device at the other one, a casing with the
bearings and a dashpot, as shown in figure 1. The au-
thors then investigate the useful turbine energy dis-
Card 2/5 sipation during oscillations. Inadequate balancing

SOV/143-58-11-15/16
-.The Influence of Experimental Turbine Vibration on the Test Accuracy
and centering of the rotor, beating of the hydraulic
brake disc and other defects in the experimental
unit may cause considerable forced oscillations of
machine elements and foundations. The authors pre-
sent formulae and equations for calculating the work
spent for these oscillations. They point out that
the accuracy of balancing is of great importance. At
BITM an experimental unit was built for determining
the power measurement errors caused by vibration. An
electric motor is used for turning the experimental
turbine rotor, as shown in figure 3. The electric
motor stator was placed in ball bearings. The moment
developed at the shaft of the motor was measured. The
friction in each of the turbine bearings was measured
by means of floating bushings. The vibrations were
caused by artificially unbalancing of the rotor by
adding small weights. The results of this test are
shown in figure 4. The mechanical losses in the bear-
ings of experimental turbines were determined at BTM
Card 3/5 by floating bushings, into which the races of the ball

SOV/143-58-11-15/16
The Influence of Experimental Turbine Vibration on the Test Accuracy
bearings of the turbine shaft were installed 92 as shown
in figure 6. At an oil pressure of 3-4 kg/cm , these
bushings begin to float and the friction moment in
the bearings is measured by means of balances L'Ref 17.
It was established that under certain vibration con-
ditions a negative f.,.,iction moment is observed and
the measurements of friction losses in the bearings
become unreliable. Investigations showed the fric-
tion moment in the bearings may be measured with ade-
quate accuracy, provided the floating bushings do not
touch the walls of the cauing. Strong vibrations may
cause a seizing of the bushings in the casing and will
cause errors of friction moment measurements. The au-
thors arrive at the following conclusiPn: 1) Vibra-
tion of experimental turbines are connected with an
additional resistance moment, originating at the shaft,
which is not measured by the brake. The magnitude of
the error caused by the additional friction norient
may attain considerable values, especially in stages
Card 4/5 with short blades and with partial admission of the

OOV/143-58-11-15/16
The Influence of Experimental Turbine Vibration on the Test Accuracy
working medium. The error may be esuential with a
great temperature drop at the turbine, regardless to
a considerable power of the experimental turbine.
2) The magnitude of the experimental error will be
especially large with small dimensions of the model.
Extraordinary careful balancing is required for small
models. 3) Some devergances of the experimental re-
sults with analogous stages on different experimental
turbines may be explained by an undercutimation of
the energy dissipation cauned by vibration. There
are 2 diagrams, 1 photograph, 3 graphs and 3 Soviet
references.
ASSOCIATION: Bryanskiy institut transportnogo maoliinostroyeniZa
Bryansk Institute of Transport Machine Building)
Rafedra turbostroyeniya (Chair of Turbine Building)
SUBMITTED: September 21, 1958
Card 5/5

POVKH, Ivan Lukich' Prinimgl uchastiye: SHIRNOV. G.T., insh.. KIRILLLOT#
I.I.J-Prof.. doktor tekhn.nauk. rateenzent; BOGDANOTI, T.T.,
.. 1T3ndf1z.-mt.nnuk, red,; SIMONOVSKIT, V.Z., red.isd-va; DUDMOTA,
G.A., red.isd-va; SHCHETININA, L.V., takhn.red.
(Aerodynamic experiments in mechanical engineering) Aerodinamd-
choskii eksperiment v anshinostroanii. Moskva. Gos.nouchno-takhn.
izd-vo mashinostr.lit-ry, 1959. 394 P. (MIRA 12:9)
(Aarodynnmice) (Mechanical engineering)

8(6) SOV/143-59-2-13/19
AUTHORS: KirillovVI64I., Professorg Doctor of Technical Sci-
encee, and Kuzlmichev, R.V., Candidate of Technical
Sciences
TITLE: The Influence of the Angle of Rotation of the Guide
Blades on the Efficiency and the Degree of Reactivi-
ty of a Turbine Stage (Vliyaniye na k.p.d. i na ste-
peril reaktivnosti turbinno stupeni ugla povorota
napravlyayushchikh lopatok5
PERIODICAL: Izvestiya vysehikh uchobnykh zavedeniy - Energetika,
1959, Nr 2, pp 101-110 (USSR)
ABSTRACT: A small turn of the guide blades of a turbine stage
changes the characteristic of the latter to a con-
siderable extent and it is used for this purpose in
practice. Thereby, the change of the degree of re-
activity has a great influence on the performance
of a turbine stage. Applying the rotation of guide
blades, the designer must have the possibility to
estimate the losses of energy connected ~yith such a
Card 1/5 turn and must be able to determine the degree of

SOV/143-59-2-13/19
The Influence of the Angle of Rotation of the Guide Blades on the
Efficiency and the Degree of Reactivity of a Turbine Stage
reactivity. In the available liternture, there are
very few experimental data, roquired for such cal-
culations. For this reason, at BITM-Bryanskiy in-
stitut transportnogo mashinoetroyeniya (Bryansk
Institute of Transportation Machine Building) a
series of experiments were performed on gas turbine
stages with different guide blade angles of rota-
tion and unchanged rotor blade position. These ex-
periments characterize the influence of the angle
of rotation of the guide blades and may be used to
evaluate the influence of the degree of reactivity
on the efficiency factor of the turbine stage. The
principal dimensions of the experimental stage are
shown by figure 1. The d/1 ratio was approximately
S. The rotor and the guide bladqs had the profiles
of the Leningradskiy metallicheskiy zavod (Lenin-
grad Metals Plant). The basic stage had gn outlet
angle of the stationary blading of_,:~-;17 . Five
Card 2/5 modifications were obtained from this basic stage

SOV/143-59-2-13/19
The Influence of the Angle of Rotation of the Guide Blades on the
Efficiency and the Degree of Reactivity of a Turbine Stage
having anglesO, - 149 15, 16, 18 arid 190 and were
designated according to the angle valuee by numbers
14 + 19. The experiments were performed with a
single-stage experimental air turbine. Figure 2
shows the system of measurements used. The methods
of the BITM gef 1 were used for obtaining and pro-
cessing the experilmental data. Besides measuring
the conventional parameters, the pressure in the
axial clearance between the rotor and the stationary
blading was measured. The experiments showed that
the energy lose factors, changesoby 0.2% when shift-
ing the guide bladlng by 14 + 19 . The authors
present the investigation results for the efficiency
factor, the degree of reactivity and the influence
of the latter on the energy losses within the sta e.
The authors come to the following conclusions: 1~
With great Ilow outlet angles, a turn of the blades
by several degrees will cause an insignificant
Card 3/5 change of the profile energy losses in the guide

SOV/143-59-2-13/19
The Influence of the Angle of Rotation of the Guide Blades on the
Efficiency and the Degree of Reactivity of a Turbine Stage
blades. 2) A small turn of the guide blades causes,
at an optimum value of u , a c-omparatively small
U-0 $
change of the turbine stage efficiency factor)-), which
was calculated under consideration of losses of kine-
tic outlet energy. The efficiency factor, calculated
under the consideration of using the kinetic outlet
energy, changes with a turn of the guide blades to
a greater extent. 3) When turning the guide blades,
considerable energy losses occur under the influence
of the angles of attack. 4) Increased degrees of
reactivity of a turbine stage are connected with a
considerable decrease of profile energy losses in
the rotor, especially in the areas of negative de-
grees of reactivity. There are 2 diagrams, 11 graphs,
2 tables and 1 Soviet reference.
Card 4/5

SOV/143-59-2-13/19
The Influence of the Angle of Rotation of the Guide Blades on the
Efficiency and the Degree of Reactivity of a Turbine Stage
ASSOCIATION: Bryanskiy institut transportnogo mushinostroyeniya
(Br ansk Institute of Transportation Machine Build-
ing~
PRESENTED: Kafedra turbostroyeniya (Chair of Turbine Build-
ing)
SUBMITTED: November 18, 1958
to
Card 5/5

8(6)
SOV/143-59-12-10/21
AUTHOR: Kirillov, I. ., Professor, Doctor of Technical Sciences
TITLE: An Equ; )n of the Radial Balance for a Turbine Stage
PERIODICAL: Izvestiya vysshi-kh uchebnykh zavedeni.y: Energetika,
1959, lir 12, PP 73-76 (UjO'R)
ABSTRACT: The author gives some propositions on an equation for the
radial. balance of the flow movin- behind the directing
apparatus and the runner, lie pro-ceeds from the equation
for balance:
C2 le
U r (1)
=t
,ahere r is the radius of the respective circle; p and
- the pressure and dei~jity respectively of the gas or
steam; t - time; dc r - radial acceleration. Derived
'M
Card 1/2 from this is the final differential equation:

SOV/143-50-12-10/21
An Equation of the Radial Balance for a Turbine Stage
dc2 c dc2
lz lu 2z
dr Z2u dr (6)
'When stages with uneven axial speeds behind the runner
are being evaluated, power losses caused by levelling
in the acceleration field must be taken into account
If the axial speed component in front of the working
wheel diminishes from the root to the periphery of the V/
stage, then an increase in the axial speed of the flow
takes place behind the wheel. There are 2 diagrams and
3 references, 1 of which is E~nglish and 2 Soviet.
ASSOCIATION: Bryanskiy institut transportnogo mashinostroyeniya (Bry-
ansk Institute for Transport Machine Construction)
SUBMITTED: August 17, 1959, by the Kafedra turbostroyeniya (Chair
of 'Nrbine Construction)
Card 212

KIRrLWY, I. I., doktor tekhn.nauk prof.,; XUZIMICHN, R.T., kand.takhno
nauk
Affect of leakages on the selection of the reactivity do-
gree of the turbine stages Izvevysouchebozavo; snerge 2
no.6:55-60 Je 159. (HIR-k 13:2)
1. Bryanskly Institut transportnogo mashinostroyenlya. Pred-
otavlena, kafedroy turbostraymnlya.
(Turbines)

I ,
KIRILWV, L, insh.; PASMY, N., Insh.; SOLOVOYN. V., insh.;
Roaderal comments on V.S.Bandarenkols article "Improve the
Inspection of boiler units.* Bezop.truda v pro= 3 no.gs
21--t24 S 159. OURA 1312:
1, Upravlonlya Savaro-Zapadnngo 6kruga Goegortekhnadsora
RSTSR (for Kirillov, Pashkov. Solov'jav). 2. Zamastitell
predeadatelya Komitats, Googortakhnadsom Aserbaydzhanskoy SSA
(for Karev).
(Boiler Inspection) (Bondaranko, V.S.)

36241
S/145/ /60/000/002/009/020
12 4109, /J912 D221/D302
AUTHOR: KiriiiRYJL~~ Doctor of Technical Sciences,
--Pr6ressor
TITLE: Experimental investigation of gas turbine stages
with different degrees of reaction and variable a
PERIODICAL: Izvestiya vysshikh uchebnykh zavedeniy. Ylashino-
stroyeniye, no. 2, 1960, 88 - 97
TEXT: A description is given of experiments on the rational selec-
tion of the degree of reaction for different work conditions of
turbines, and made with different exit angles a,. The degree of
reaction was calculated as the ratio of thermal drop of potential
in the rotor to the total drop in the stage, and it showed an in-
crease fron -0.6 to +0.14. Changes in a, produced significant in-
cidence angles of flow past the blades which were not modified,
whereas during design this can be taken into consideration. The tX
coefficient of efficiency exhibited a fall with the reduction in
the deCree of reaction. Experiments were carried out with a con-
Card 1/4

30241
S/145/60/000/002/009/020
Experimental investigation of ... D221/I))02
stant height of blades. In actual design, these -ire also varied
with the an6ie a1 as the gas flow remains approximately unaltered.
Reduction of reaction loweres the coefficient of efficiencyt when
higher blades produce an improveL:cit.Tests on r1odels (A and B)
were made in order to compare the efficiencies of stages. Rotor
blades of both had the same profilc3, and results were almost iden-
tical. Coi~ipari8on with models of different root diametersp but
with equal height of blades indicated a drop of efficiency for low-
er reaction which had a greabarrate thar, in the case of charged
angle ale Two models with a higher ratio of reaction (D and C) werZ,,/
then tested. The optimum coefficient of efficiency was obtained
with a larger ratio of reactionp and the curve was steeper, The
anlge of flow in turbine C was greater than in D, and this caused
additional lose of power. When considering results of experiments#
special attention was drawn to the degree of reaction in the root
section; although other sections are also important. Howeverp the
stream has a greater turning near the rcot section of the rotor,
where maximum losses are incurred. The examination demonstrated
Card 2/4

30241
S/145/60/000/002/009/020
Experimental investigation of D221/D302
that an increase of reaction in the negative region improves stage
efficiency, No break of flow was observed in that zone even at a
low ratio of reaction. The stability is explained by rapid increa-
se of reaction with a rise of radius, and by the fact that more
distant layers of flow deliver kinetic energy to the gas which
passes through the diffusor part of the channel. Centrifugal for-
ces in the boundary layer produced by rotation of a wheel also
have a favorable effedt. Operation of a stage with a small positi-
ve or a negative ratio of reaction hz,~s advantages, because its
root (''iL~Lieter is reduced, or the worked thermal potential is hjgher.
This 6ivcs ground for continuing the work on improving stages with
a low ratio of reaction. The latter method should not be used when
rotors have unloading holes which may produce an opposite flow of
gas. The author considers that in the case of two-shaft gas tur-
bines it is expedient to use slewed guide blades in the upstream
of the main turbine, when operating at part loads. The latter cause
an increase of temperature which improves efficiency. Experiments
proved that 1 - 20 turning of blades from the position of optimum
conditions produces only a small deterioration of efficiency.
Card 3/4

4 1
8/145/60/000/002/009/020
Experimental investigation of D221/D502
Theia are 9 figures and 4 Lcoviet-bloc references.
ASSOCIATIOL': Bryanskiy institut transportnogo mashinostroyeniya
(Bryansk Institute of Transport Engineering)
SU-]7jITTED: December 15, 1959
Card 4/4

83850
s/l14/6o/ooo/oo9/ool/OO7
0 E191/E481
AUTHORS: ...Kirilloy I j-T---npctor of Technical Sciences, Professor
And Kirillov, A.I., Engineer
TITLE3 Turbine.Stagea Which Develop a Large Starting Torque
PERIODICAL: Energomashinostroyeniye, 1960, No.9, pp.6-8
TEXTi In gas turbine plants for traction applications, a turbine
with a large starting torque can simplify the transmission of the
ma...n drive and thereby significantly improve the efficiency and
reduce the cost of the entire installation. Some analytical
derivations and tests carried out at the Bryansk Institute of
Iransport Machinery (Bryanskiy institut transportnogo
mashinostroyeniya) are reported which illustrate the possibilities
of greatly increasing the starting torque in stages especially
designed to this and and thus deviating from other optima under
operating design conditions. The factor by which the starting
torque exceeds the operating torque under design conditions can be
calculated in the first approximation assuming an unchanged gas mass
flow and becomes a function of the circulation coefficient only.
Tests have shown that the measured starting torque is higher than the
values so calculated and it is necessary to study the flow through
Card 1/3

83859
S/114/60/000/009/ool/007
Eigi/E481
Turbine Stages Which Develop a Large Starting Torque
blade cascades at very large incidences. Tests of a plane
cascade of rotor blades were carried out at a Reynolds number of
250000 and a Mach number of 0.2. The main object was the
evaluation of very large positive incidences on the profile losses
in the cascade and on the outlet angle. With a rising incidence,
starting from 20*, the velocity coefficient drops sharply. In the
beginning of this region, the kinetic energy of the impinging flow
is still large and the cascade losses are increaseds When the
inlet angle approaches 900, the relative magnitude of the inlet
kinetic energy falls to a minimum because the free cross-section
becomes a maximum. The rate of decrease of the velocity
coefficient becomes smaller. The outlet angle on the other hand
remains almost constant between zero incidence and an incidence of
0
about 80 . The outlet angle slightly diminishes with a further
increase of incidence. Tests of two succeeding plane cascades,
Simulating the stator and rotor blades, have shown that, by
increasing the axial clearance between the cascades, the energy
losses can be reduced. In annular cascades, the pressure
distribution is different and the effect of the axial clearances
Card 2/3

83.350
S/114/60/000/009/ool,'007
El9l/E48l
Turbine Stages Which Develop a Large Starting Torque
requires further investigation. The preliminary tests so far
reported indicate the possibility of designing gas turbines for
transport application with a high starting torque. As shown by
the tests, the high incidences occurring at standstill are
compatible with satisfactory continuous operation of the stage.
The large resistance of the cascades at standstill causes an
increase in the degree of reaction which determines the mass flow
through the turbine. There are 7 figures and 3 Soviet references.
Card 3/3

KIRILLOVj,.I,I-.j,doktor tekbn.nauk
Deviation from the criterion of static autonomy in systems
controlling sever&1 values. ToploonGrgatika 7 no-9:4S-55
6 160. (MIRA 14..g)
1. Bryanskiy institut transportnogo mashinostroyeniya.
(Stem turbines)

-1 - ,
S/M?P10100010 10/006/011
C2 Al 69/A026
AUTHORs Kirillov, I. I. ---Doctor of Technical �'CiOn~es, ro~es_~qr_
TITLE: Investigation of the control dynamics of turbines with inter-
mediate steam superheating using a frequency method
PERIODICAL: Energetikaj no. 10$ 1960, 53-66
TEM The author investigates the influence of the intermediate re-
heating stage.upon the stability and transient response of the turbine con-
trol system. The investigation is carried out with the use of a frequency
method described by Professor V. V. Solodovnikov in (Ref, 31 0snovy avtoma-
ticheskogo regulirovaniy-a (Principles of Automatic Control), Mashgiz, 1954).
The block diagram of the turbine control ByRtem, shown in Figure 1, is trans-
formed to include an equivalent link M representing the vclume of the inter-
mediate reheating stage. The theoretical analysis of this control system in-
dicates that an improvement of the control stability can be obtained with a
large volume of the intermediate reheating stage. In many ca3es, the least
favorable operating conditions for control stability exist at small turbine
loads. Figure 3 shows frequency response of the equivalent intermediate
Card 1/5

20308
3/143/60/000/010/006/011
Investigation of the control dynamics ... A169/AO26
volume. Figure 6 shows the real frequency response of a closed-loop control
system relative to the perturbing action. Figure 7 shows the transient con-
trol response of this 9yatem. There are 7 figures and 3 Soviet references.
ASSOCIATIONt Bryanakiy institut tranaportnogo mashinostroyeniya (Bryansk
Institute of Transportation Machinery)
PRESENTED: Kafedra turbinostroyeniya (Department of Turbine Building)
SUBMITTEDs Juno 11, 1960
Card 2

of the control dynamics...
0 at 42 43 44 "1 47
-42
-05
20308
S/143/60/000/01o/bo6/bil
A189/AO26
98 40 to
Rw -0
ft 1,6

Rjw 13
.44

103
Firure 3 Frequency rouponse of equivalent intermediate volume
Card 3/5

Investigation of the control d:ynamiae...
20308
311431601000101010061011
A189/A026
3

V,

Figure 6:
Real frequency response
of closed-loop control
system
13, CS
Card 4/5

Inve.,itigation of thu control dynanica...
A
R

.0

8
S/143 60 00101010061011
A189 A026
Fipure 7t
Transient control response
Card 5/5

PHME I BOOK EUWITATIOK SOV/5756
Kirillov, Ivan Ivanovich
Avtonaticheakoye regulirovaniye partvykh i gazovykh turbin (Automatic Control of
Steam and Gas Turbines) Moscow, Mashgiz, 1961o 599 P, Errata slip Inserted.
7000 copies printed*
Reviewer: SP. Kuvshinnikov, Engineer; Ed*: N.L. Raykhell, Candidate of Techni-
cal Sciences; Ed. of PuLb3ishIng House: A.A. Basentayan; Tech* Ed*: TeFo
Sokolove.; Managing Ed. for Literature on Heat Energy, Metallurgy, Highway
Construction, and Hoisting and Transporting Machinery Construction: G.I.
Baqdakov, Engineer.
PURPOR: This book is intended for engineers concerned with the Investigation,
design, and operation of steam and gas turbines and other types of turbo-
machinery. The book may also be useful to students taking courses in turbo-
machine control at schools of higher education.
COVERAGEt The book gives a systematic presentation of the theory of steam- and
gas-turbine control, analyzes modern control systems, and discusses special
Card l/

Autcmatic Control of (Conte)
SOV/5756
design features of the elements of these systems, Particular attention is
given to problems of control dynamics. Many problems in the dynamics of
steam and gas turbine control are Investigated vith the aid of frequency
characteristics. No personalities am mentioned. There are 135 references:
Ln- Soviet, 6 German, and 2 English.
TABIZ OF CCWBMM:
Forevord
B&sie Symbols
Introduction
3
5
7
Ch. I.- Regulators 16
1. Cheracterietics of centrifugal regulstors 16
2. Caaculatior and construction of centrifugal regulators 30
3. Pressure regulators 39
9,r& 2/7

KIRILLOV, I.I.
- Air curtains of induetrial enterprises.
27-29 Ja '(1,
(Air curtains)
Vod. i san. takh. no.l:
(MIRA 14:9)
k

30284
S/096/61/000/012/001/003
E 19 4 /E 15 5
AUTHORS: _Kiri1lov_t__jj., Doztor of Technical Scaences, and
'N_r_ei_hW4~vj A.A., Engineer
TITLEj Turbine stage having guide channels with flat walls
PERIODICAL: Teploenergetika, no.12, ig6i, 45-51
TEXT: A turbine stage in which the surfacesbounding the guide
vanes are cylindrical has the disadvantage of relatively high
energy loss at the stage roots because of flow over a curved
surface, and leakage of working substante through the pert.phery of
the open axial gap. Stages of this type are termed cylindrical.
Other stages which have long been used have the guide vane dutts
bounded at the root and periphery by flat surfaces, usually
produced by straight milling of the blades. These will be termed
flat-ended stages; the flow in them is guided by the flat ends of
the blades and so their characteristics differ from those of
cylindrical stages, For example, in theory one would expe:t a
constant degree of reaction along the blade radius, Work was
undertaken at the Bryanakiy inatitut transportnogo mashinostroyeniya
(Bryansk Institute of Transport Engineering) (BITM) to Lompare the
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Turbine stage having guide channels S/096/6 1/00010 1 2j/00' /001,
EigVEilr-t-
characteristics of cylindrical and flat-ended stages, with blades of
medium height. The stages are illustrated d4agrammatiz-ally in
Fig.1, where the uppermost diagram (a) shows the flow path, whi--h
was used in all cases. The diagram 6 shows a mod~tl 2 gu_,de -.rant
and the d1agram 8 gives two views of the model 2 g,_xide-blade
arrangement, Model I was a cylindrical stage, nct ITI
which the top and bottom of the guide -oanes were cyl:ndrica!,
whilst, as will be seen from the diagram, An model 2 ,he guide
blades had plane-parallel ends. All the models used the samp rot-or
with strip shrouding. Both models used the same blade profLle~
The tests were made on a single-ata e air turbine with conditions
of M,:,I;~',0.33 and Recl rJ 4.11; x 107. Each model was tested with
se-eral values of open axial clearanco 61 in the range 0.5-5 mm,
in order to assess the influence of the leakage of work.-.ng
substance through the peripheral axial gap. F,!A'icen~y survas arr
given in Fig.2; the curves in Ftg.2a relaie to Model 1 anJ thos,~-
in Fig,2C to Model 2. Fig.3 shows rea-tion cur-zes a-. the roo'.
(e') and at the periphery (p # ai fun-.tions of lhz-
u/C. for various values of clearan,-e 61 The d.-tts-d !_ns,.-ii
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30284
Turbine stage having guide channels ...
s/oq6/61/000/012/001/003
z194/EI55
relate to Model 1 and the bold lines to Model 2. 11,1odel I has
normal characteristics for an active type stage with untwisted
blades. Model 2 has very different characteristics; the degree
reaction is almost constant over the height of the flow path, an
would be expected from theoretical considerations. This is true
over the whole range of speed and clearances studied. The degree
of reaction on the mean radius of Model 2 was much less than for
Model 1, particularly for small axial clearances. The efficiency
curves for Model 2 are also very different from those for Nodel I
In particular, the efficiency of Model 2 is higher, both when the
clearance 61 is big and when it is small. Flow, pressure and
speed measurements across the stages showed that the distribution
was uneven in both models, but more even In 'Model 2 than in Model
the kinetic energy of discharge was also lower. With Model 2 the
leakage of working substance through the open axial gap is lower,
because of the reduced reaction at the peripheral section.
Moreover, the degree of reaction at the mean section can be lower
than with Model 1, nnd this has the usual advantages.
There are 7 figures and 5 Soviet-bloc references.
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30284
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Turbine stage having guide channels ... E19VE155
ASSOCIATION: Laningrodskiy politokhnichoskiy instittit
(Leningrad Polytechnical. Infititute)
Card

Fig.2

KIRI L16V 1. 1. , doktor takhn. nauk g prof GOC~ILEV , 1. 0. , kand. tekhn. muk
dotoant; DMIONOV, R.I.,, kand.tekhn.neuk; KLIMMOV, A.A., lnzb.
Aerodynamio study of the outlet nozzle of a gao turbine.
Izv, vyo* uchebe zavej,enarg. 4 no*8:56-59 Ag 161.
(mm 14:8)
1. Bryanskiy institut transportnogo mashinostroyeniya.,
Pradstavlena kafedroy turbostroyeniyu.
Ow turbines)
V

KIIULLOV, I.I., doktor tekhn.nauk, prof.; IVAIJOV, V.A., inzh.
Frequency analysis of a certain class of equivalent links. Izv.
vys. ucheb. zav.; energ. 4 no.10:6o-67 0 1(1- OURA 14:13)
1. Leningrad4.iy politekbnicheskiy institut Imoni H.I.Winina.
Predstavlena kafedroy turbinostroyenlya.
(Automatic contr:)I)

KMII&)V. I.I., doktor tekhn.nauk,,prof.$,YABIDNIK, R.M., kand.takhn.nauk,
*~ ---d-oteent
Characteristics of tiwbine stages at different pitch angles of
the guide blades. Energomashinostroonle 7 no.6:7-3.1 Js 161.
(MIM 14:7)
(Gas turbines) (Steam turbines)

KIRILLOV, I.I., doktor tekhn.nauk, prof.
Effect of the shape of the blading of the low pressurf- eri,~ on the
efficiency of steam turbines. Ener,-omashinostroenle 7 na.12fl-5
D 161. (MIRA 14:12)
(Steam turbines--Testing)
4

23554
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1.19. A22 0 E194/E155
AUTHOR: Kirillov, I.I., Doctor of Technical Sciences
TITLE, Changes in the torque of a gas turbine stage as
functions of the speed of rotation
PERIODICAL: Teploenergetika, 1961,1 No-7, PP. 18-24
J
TEXT: This article considers the characteristics of turbine
stages when the inlet and outlet gas conditions are constant.
The influence of changes in rate of gas flow and heat drop on the
torque can easily be allowed for. The main parameters that
determine the torque when the ratio u/CO (runner peripheral
speed/gas velocity) is small are first considered theoretically.
The following expression in derived for the starting torque of the
turbine:
)I = X2 + 1 (6)
H H cuo
where: PH is the torque wh i the runner is stationary; u = 0;
XH in the flow factor when u = 0; cuo a the circulation
factor under rated conditions. It in st!ted that in order to
have high torque on starting and at low speeds the stage should
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2355
s/o96/6I/oo5007/001/UUO
Changes in the torque of a gas E194/EJL55
have a low value of circulation coefficient cuo under designed
conditions and a high flow-factor at low speeds. It is most
important to choose the right kind of 3tage for different types of
gas turbine if high starting torque is to be obtained without
attendant disadvantages. The influence of low circulation-factor
on blade design in discussed; it is usually necessary to use
blades with large angles of attack and profiles that are not
sensitive to differences in the angle of attack. The problem of
designing turbines to operate over a wide speed range can be
tackled in many different ways and in order to make a correct
choice of the type of stage the designer requires access to
experimental data on power losses and flow factors for stages of
different types. The article then gives test results of this kind
for stages of the active and reactive types. Both of the stages
tested had relatively long twisted blades. The active stage (A)
had a maximum efficiency of 0.60 and reactive stage (R) 0.65.
Stage (A) was tested in air in the range of Reynolds numbers
2~9-3.3 x lo5 and stage (R) in the range 2.5-3 x 1o5. During the
test measurements were made of the iunning speed, the shaft
torque, the air flow, the inlet and discharge air conditions, and
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Changes in the torque of a gas E194/Ei55
the pressures at the blade roots and periphery. The pressure and
velocity distributions were also measured, at a distance of 4-5 mm
from the discharge edges. Pressures'were also measured in various
places. Fig.6 shows the relative torque p and flow factor X
as functions of u/CO for stage (A). It will be seen that the
torque in 2.4 times the rated value when the runner is stationary.
The flow factor rises steadily an the speed in reduced, reaching a
value of 1.062 when the runner in stationary. A certain difference
between the theoretical and practical values of starting torque was
explained by changes in the mean angle of di.scharge of flow from
the runner when stopped as compared with the angle under optimum
conditions. Fig.10 shows curves of the torque p and the flow
factor X an functions of u/CO for the reactive stage (R).
It will be seen that when the runner is stationary the starting
torque is 2.5, which in in good agreement with the value of 2.42
calculated by Eq. (6). With the reactive stage the starting torque
was slightly higher than with the active, but the angle of attack
at starting was considerably greater though the conditions of flow
over the blades were somewhat better. The change of.reaction with
speed is, of courseq quite different in stages (A) and (R).
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Changes in the torque of a gas turbine ... E19VE155
It is concluded that the static torque depends mainly on the value
of the circulation coefficient =U0 under rated conditions, and on
the flow factor )( when u = 0. The approximate formula (6)
is recommended for calculating starting torque.
There are 10 figures and 2 Soviet references.
ASSOCIATION: Bryanskiy institut transportnogo mashinostroyeniya
(Bryansk Institute of Transport Engineering)
Card 4/5

YIRILIXV) I.I. , doktor t,3khn.rav.':; IT'J.'OV, 7".A.) imb.
Stability and trancient rerulation procozoo ef turbinoz with
intermediate steam reheating. Toplooner-All-a ". no.10:55'
60 0 161. L, 14:10)
1. Loningradakiy polite'Inichen"i institut.
(Stor-n titr*binoo~

KIRILLOV doktor tekhn.nauk; TERESHKOV9 A.A.j Inzh.
. -iLl-.
Turbine stage with flat wall guiding channels. Teploenergetika 8
no-M45~-51 D 161. (MIRA 14t12)
1. Leningradskiy politekhnicheakiy institut.
(Steam turbines--De3ign and construct'-on)

. 1.
ZYSIN, Vladimir Aronovichl KIRILIDI , retsonsentl
ERLIKA, V.A.p SOBOLEVA, YOX, tokhoo red.
(Composite steam-gas systems and their operating cycles]
Kombinirovannye parogazovys ustanovki i taikly. Moskva
Gosenergoisdat, 1962. 185 p. (MIRA 16:51
(Thermodynamics) (Electric wer plants)
(Heat-Tranamissionr

37859
/P 6
0
S/143/'2/000/005/003/003
D238/D308
IXTMIS 'Z"irillov, I.I., Doctor of Technical Sciences, Gogolevt
R.O., Candidates of Technical Sciences,
and Klimtsov, A.A., Engineer
`2 1 T L The BITM exporimenltl-al air turbines
P 3R. 10 D I C!, LIzvestiya vysohikh uchebnylx,-h zavedeniy. Energetika,
no. 5, 1962, 119 - 122
Seveial plants are available in the BIT.": for acro-dynamic in-
ve_vk1,-iGatijns on stleam and ras turbine stage models at low speeds.
0
je.-iment-al plants
for hij;h speads, already o-perating or in
construction, are described. 7.Ultiple experimental turoines have
bc!en constructed for stages in-line providing tests on either one or
t-wo stages. The turbines were desiEned so as to Provide a flexible'
ei.peri-mental test rig suitable for various investigations. A second
.7--s built into the rig for this purpose on which a second work-
inr- disc could be mounted. In ihis way both rotors could be connec-
teud by a flexible shaft and measurements taken of the total torque,
or each disc could be connected with its hydraulic brake and measu-
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S/143/62/000/005/003/003
The DIM. experimentai air turbines D238/D308
red separately. Tests could also be carried out with mutt:ally oppos-
n6 ro'a--on. The second frame can be set up at different distances
.Lro,,,i the first, affording tests with different, transitions between
Vhe wi4L-.h a different stage admission. This is important
when investiGatinG the flow after the regulation sta~-,e. investiga-
tions can also be carried out on the inlet and outlet nozzles opera-
to.`A.nG simul-taneously with the turbine st-a-e. Im experimental turbine
-u U
has been designed also for testing the stages of large s-Cleam and gaa
turbines at high acoustic velocities. The turbine is designed for
operating up to 12,000 r.p.m., developing a power of 200 kV1. -2xpe-
rience has shown that universal experimental turbines a.re com-plica-
ted ~cnd expensive in operation. Relatively simple experimentai t-urbi-
nes should be fitted up for solving particular p.-oblems. Test rigs
are recommended affording a number of standard units. There are 5
f-4.-r-ures and 2 .1joviet-bloo references.
A.S-OCCIATION: Bryasnkiy institut transportnogo mashinostroyeniya
(Bryansk Institute of Transport Vlachine Construction)
SUB".:ITTED: September 20, 1960
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D234YI)308
AUTHURS: Kirillov,.--I.I. and Kuzlmichev, R.V.
TITLZ;': Energy losses in a turbine stage due to fastening
wires
P"_RIODICt%L: Referativnyy zhurnal, Mekhanika, no. 1, 1963, 369
abstract 13212 Mektr..stantsii, 1962, no. 7,
38-42)
TM!: The authors give the reaults of an experimental in--
vestigation of aturbine stage with one, ti-io and three rows of fast-
ening wire on working blades.
f-Abstracter's note: Complete translati6n2
S/12 631000100110131080
Card 1/1

GALKIN, XURBET, S.A.; KIRM=V, L.I.
Design of machinerv and the cost of its production.
khozmsh.32 no.7t25-27 J3. 162.
(Agricultural machiner7)
Trakt. i sell-
(MIRA 15-7)

KMLLCVj I I doktor tekhn.nauk, prof.; YABLONIK, R.M., kand.tekhn.naukp
dotment
Effect of supercooling and constitution of vet steam on its
expenditure by nozzles. Energomashinostroanie 8 no.10:6-10
0 162.
(HIRA 15:11)
(steam)
(Steam turbines)

%XIRILLOV I I doktor tokhn. nauk, prof.; ZTSIN, V. A., kand. tekba.
MU-=--t4l
naukI OSHEROV9 S. Ta., kand. tekhn. nauk
Problem concern ng the coolinst of a high-temperature gas
turbine. &ergamashinostroenie 8 no.12:7-10 D 162.
(MM 16:1)
(Gas turbines-CoolinR)

KI-RILLOV,_I.I., doktor tekhn.nauk,- TABLONIK, R.M., kand.tekhn.nauk
Problem of the improving of turbine stages operating with moist
steam. Teploonergetika, 9 no.1014l-47 0 162. (KRA 15%9)
(Steam turbines-Design and construction)

VOSHCHANOV, Konstantin Pavloviehl KIRILWV. lyn I mnoviobi CHEFEYAKV.S.,
nauohnyy rod.1 SAZIKOV,, M.I.,, red.1 DORODNOVA, L.A., tekhnered.
(Machines and apparatuses for the flame machining of metals]
Mashiny i apparstura. dlia gazoplamennoi obrabotki metallov,
Moskva, Proftekhizdat, 1963. 122 p. (MIRA l6s6)
(Gas Yalding and cutting-Equipment and supplies)

S/c96/63/000/002/004/013
E194/E455
X01 H( it 3: Kiritlov, I.T., Doctor or Technical sciences, Professor,
17t-i-t i i T s-o-v-, 7It g I n e a r
I ITI-E Vnergy 3cismax In shrouded and unshrouded turbine stages
I t;1!)voJ(AL: Tutilotinerget1ka, no.2, 1963,.3c-35
X'j '.Oiem peripheral speeds are high. it in necensary to
detet-mine whether tile ndvantages of shrouding Justify tile
tir-ictical cumcutties which it introduces. Hatica it is necessary
to accurately the influence of shrouding on stage losses.
'file o1cl Andwrburg and Brown-Bovert formulae are based on reaction
ancl so can p-ive false result-s. More recent work relates,
0., ot.hvr wore al)Isropriate types of stayc but the test results are
con ( rAd 147 tOt-Y. Accordingly, tests were made in an experimental
tili-biiif: iu.-ing shroudell and unmilrouded mtages, most of' tile impulse
tyiin, :iomc with ti-efisted blades, . Ctirves are plotted of efficiency
I'mictioits of' velocity ratio and of radial -cleArallce 6 1 ' f1OW
chir,ictcristlcn m-ar tile blades were determined. It was found
th,it- iii unsitrostrN.-d stages, blade tip lesson are little Influenced
by (fie amount o(' reaction at tho peripheral section, because
inci-oa.--ed reaction Increases leakage through tho radinI clearance
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n t: r gy I oss e a Lt94/E455
but re(113cos secondary losses of various kinds and vice versa.
Consequently, in such stages losses associated with radial
c1cai-ance may be significant even when the peripheral section
reaction is low. Unshrouded impulse blading !Eith smooth flow
pixth at the periphery has high tip losses if 6 > 0*005;
these lonses may be reduced by employing guide vanes with positivo.
peripheral overlap. With the radial clearances normally used, the
presciice of shrouding significantly improves tho efficiency of
impulse blading. Moreoveri with shrouded blading the.radial
clearance may be somewhat reduced. Accordingly, shrouding should
be used whenever possible. There are $ figures and I table,
ASSOCIATIONS: LIII - DIDI
Card 2/2